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 58466U 26145.51084880 +.00000000 +00000-0 +22999-3 0 00008
2 58466 97.3493 213.1874 0013808 38.9531 321.2702 15.30864490 08
| Epoch (UTC): | 25 May 2026 12:15:37 |
| Eccentricity: | 0.0013808 |
| inclination: | 97.3493° |
| perigee height: | 464 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 213.1874° |
| argument of perigee: | 38.9531° |
| revolutions per day: | 15.30864490 |
| mean anomaly at epoch: | 321.2702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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