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 58302U 26145.60067953 +.00000000 +00000-0 +70107-3 0 00003
2 58302 97.3801 229.5860 0007889 264.0034 96.0318 15.50187427 08
| Epoch (UTC): | 25 May 2026 14:24:58 |
| Eccentricity: | 0.0007889 |
| inclination: | 97.3801° |
| perigee height: | 411 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 229.5860° |
| argument of perigee: | 264.0034° |
| revolutions per day: | 15.50187427 |
| mean anomaly at epoch: | 96.0318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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