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 62051U 26145.41356407 +.00000000 +00000-0 +48412-3 0 00007
2 62051 43.0007 190.4546 0001100 275.4382 84.6344 15.27591414 00
| Epoch (UTC): | 25 May 2026 09:55:31 |
| Eccentricity: | 0.0001100 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 190.4546° |
| argument of perigee: | 275.4382° |
| revolutions per day: | 15.27591414 |
| mean anomaly at epoch: | 84.6344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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