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 61682U 26145.26178075 +.00000000 +00000-0 +21840-3 0 00008
2 61682 53.1597 95.0814 0001222 75.9430 284.1706 15.30229550 07
| Epoch (UTC): | 25 May 2026 06:16:57 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.0814° |
| argument of perigee: | 75.9430° |
| revolutions per day: | 15.30229550 |
| mean anomaly at epoch: | 284.1706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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