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 62807U 26145.46000811 +.00000000 +00000-0 +51410-3 0 00008
2 62807 53.1596 312.9093 0001434 93.0968 267.0197 15.30206085 00
| Epoch (UTC): | 25 May 2026 11:02:24 |
| Eccentricity: | 0.0001434 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.9093° |
| argument of perigee: | 93.0968° |
| revolutions per day: | 15.30206085 |
| mean anomaly at epoch: | 267.0197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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