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 28061U 26017.81075823 +.00000000 +00000-0 -39373-5 0 00001
2 28061 99.5637 48.7946 0145082 242.5324 116.1024 13.97741677 05
| Epoch (UTC): | 17 January 2026 19:27:29 |
| Eccentricity: | 0.0145082 |
| inclination: | 99.5637° |
| perigee height: | 796 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 48.7946° |
| argument of perigee: | 242.5324° |
| revolutions per day: | 13.97741677 |
| mean anomaly at epoch: | 116.1024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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