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 62893U 26145.58278132 +.00000000 +00000-0 +36618-3 0 00002
2 62893 42.9962 251.2892 0001160 269.7015 90.3704 15.27594587 05
| Epoch (UTC): | 25 May 2026 13:59:12 |
| Eccentricity: | 0.0001160 |
| inclination: | 42.9962° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.2892° |
| argument of perigee: | 269.7015° |
| revolutions per day: | 15.27594587 |
| mean anomaly at epoch: | 90.3704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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