OBJECT BN

Zdjęcie OBJECT BN

51044
Numer w katalogu Spacetrack
2022-01-13
Wyniesienie na orbitę
263.78 km
Wysokość średnia
27902.39 km/h
Prędkość średnia


Informacje o satelicie OBJECT BN

Nazwa w katalogu Spacetrack OBJECT BN
Wyniesienie na orbitę 2022-01-13
Deorbitacja
Miejsce startu AFETR (Kennedy Space Center/Cape Canaveral, USA)
WWW Tutaj
Kategorie
Perygeum 523 km
Apogeum 536 km
Wysokość OBJECT BN 263.78 km

Informacje o OBJECT BN

Demonstrate Internet of Things. \r\n\r\nChallenge is the lack of frequency bandwidth for data communication. Key features implemented in payload:\r\nAuto recognition - find the registered GS by satellite itself. \r\n Auto frequency allocation assigned by the connected GS. \r\n Handover mechanism from one GS to another. \r\n \r\nOdysseus Space is providing pre-launch testing and arranging launch services.\r\n\r\nThe mission of the LoRa receiver (433.365MHz) is to collect weak LoRa signals from the ground terminals of amateur radio operators. In order to understand the issue of Doppler frequency shift and path lose, so that the ground signal can be measured on the uplink, stored and forward issue IRIS-A also provide FM voice transponder, allowing the operator to have both digital and voice operation modes. The students can learn to understand about each sub-system of satellite. The issues of Doppler frequency shift have always plagued the applications and creativity of amateur radio operator. Here, The LoRa payload receivers receive signals, through the Store and Forward, all Ham radio operators can have more creativity and application. According to the LoRa standard parameter settings we provide, Ham radio operator upload the data to IRIS then able to get uplink data from IRIS-A website through the store and forward function. In addition. The IRIS-A also provide FM voice transponder, allowing the operator to have both digital and voice operation modes.

Satelitę OBJECT BN wyniesiono 13.01.2022r. Średnia wysokość OBJECT BN to 263.78 km. Prędkość średnia OBJECT BN wynosi 27902.39 km/h. Inklinacja OBJECT BN satelity to 97.32°.


Średnia wysokość orbity OBJECT BN

Średnia prędkość OBJECT BN

Średnia inklinacja OBJECT BN

Data aktualizacji: 2025-06-12
Średnia wysokość OBJECT BN wynosi: 263.78km
Średnia prędkość OBJECT BN wynosi: 27902.39km/h
Średnie nachylenie orbity OBJECT BN wynosi: 97.32°
OBJECT BN został wyniesiony na orbitę w dniu 2022-01-13