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 55823U 26145.36122800 +.00000000 +00000-0 +87488-5 0 00006
2 55823 87.9179 279.0525 0001566 88.1777 271.9535 13.20867522 00
| Epoch (UTC): | 25 May 2026 08:40:10 |
| Eccentricity: | 0.0001566 |
| inclination: | 87.9179° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 279.0525° |
| argument of perigee: | 88.1777° |
| revolutions per day: | 13.20867522 |
| mean anomaly at epoch: | 271.9535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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