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 58259U 26145.50786582 +.00000000 +00000-0 +38443-3 0 00006
2 58259 97.3846 229.9180 0005934 241.6013 118.4637 15.42240666 03
| Epoch (UTC): | 25 May 2026 12:11:19 |
| Eccentricity: | 0.0005934 |
| inclination: | 97.3846° |
| perigee height: | 435 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 229.9180° |
| argument of perigee: | 241.6013° |
| revolutions per day: | 15.42240666 |
| mean anomaly at epoch: | 118.4637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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