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 62617U 26145.58949126 +.00000000 +00000-0 +94721-3 0 00003
2 62617 97.3861 232.7821 0002196 53.9408 306.2048 15.51297689 06
| Epoch (UTC): | 25 May 2026 14:08:52 |
| Eccentricity: | 0.0002196 |
| inclination: | 97.3861° |
| perigee height: | 411 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 232.7821° |
| argument of perigee: | 53.9408° |
| revolutions per day: | 15.51297689 |
| mean anomaly at epoch: | 306.2048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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