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 54807U 26144.99100094 +.00000000 +00000-0 -13179-4 0 00002
2 54807 53.2155 46.2207 0001338 94.3009 265.8136 15.08844190 09
| Epoch (UTC): | 24 May 2026 23:47:02 |
| Eccentricity: | 0.0001338 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 46.2207° |
| argument of perigee: | 94.3009° |
| revolutions per day: | 15.08844190 |
| mean anomaly at epoch: | 265.8136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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