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 53058U 26145.46765194 +.00000000 +00000-0 -48071-4 0 00009
2 53058 97.4470 325.4592 0002568 104.9250 255.2261 15.05656350 05
| Epoch (UTC): | 25 May 2026 11:13:25 |
| Eccentricity: | 0.0002568 |
| inclination: | 97.4470° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 325.4592° |
| argument of perigee: | 104.9250° |
| revolutions per day: | 15.05656350 |
| mean anomaly at epoch: | 255.2261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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