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 62125U 26145.18327502 +.00000000 +00000-0 +10271-2 0 00008
2 62125 43.0024 64.5323 0001701 263.5416 96.5242 15.27606388 04
| Epoch (UTC): | 25 May 2026 04:23:54 |
| Eccentricity: | 0.0001701 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.5323° |
| argument of perigee: | 263.5416° |
| revolutions per day: | 15.27606388 |
| mean anomaly at epoch: | 96.5242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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