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 57682U 26145.55248253 +.00000000 +00000-0 -30377-4 0 00008
2 57682 53.1596 209.9960 0001510 87.9858 272.1316 15.30194312 07
| Epoch (UTC): | 25 May 2026 13:15:34 |
| Eccentricity: | 0.0001510 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.9960° |
| argument of perigee: | 87.9858° |
| revolutions per day: | 15.30194312 |
| mean anomaly at epoch: | 272.1316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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