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 58042U 26145.51987480 +.00000000 +00000-0 +36161-4 0 00003
2 58042 53.1615 78.8868 0001201 93.8284 266.2854 15.30195017 00
| Epoch (UTC): | 25 May 2026 12:28:37 |
| Eccentricity: | 0.0001201 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.8868° |
| argument of perigee: | 93.8284° |
| revolutions per day: | 15.30195017 |
| mean anomaly at epoch: | 266.2854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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