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 58101U 26145.43738730 +.00000000 +00000-0 +18337-4 0 00007
2 58101 53.1590 168.9333 0001107 96.6134 263.4993 15.30192429 03
| Epoch (UTC): | 25 May 2026 10:29:50 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9333° |
| argument of perigee: | 96.6134° |
| revolutions per day: | 15.30192429 |
| mean anomaly at epoch: | 263.4993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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