View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 44835U 19079D 24239.08914493 .13719927 28148-5 11897-3 0 9994
2 44835 97.7078 12.4018 0012883 266.2390 93.7441 16.51465352261386
| Epoch (UTC): | 26 August 2024 02:08:22 |
| Eccentricity: | 0.0012883 |
| inclination: | 97.7078° |
| perigee height: | 127 km |
| apogee height: | 144 km |
| right ascension of ascending node: | 12.4018° |
| argument of perigee: | 266.2390° |
| revolutions per day: | 16.51465352 |
| mean anomaly at epoch: | 93.7441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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