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 26020.31616294 +.00000000 +00000-0 -72778-4 0 00008
2 28061 99.5634 51.4034 0145222 235.7245 123.0094 13.97741467 04
| Epoch (UTC): | 20 January 2026 07:35:16 |
| Eccentricity: | 0.0145222 |
| inclination: | 99.5634° |
| perigee height: | 796 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 51.4034° |
| argument of perigee: | 235.7245° |
| revolutions per day: | 13.97741467 |
| mean anomaly at epoch: | 123.0094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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