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 52158U 26145.46368416 +.00000000 +00000-0 +20868-3 0 00007
2 52158 97.8233 222.1795 0011763 44.8038 315.4125 14.84986769 01
| Epoch (UTC): | 25 May 2026 11:07:42 |
| Eccentricity: | 0.0011763 |
| inclination: | 97.8233° |
| perigee height: | 605 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 222.1795° |
| argument of perigee: | 44.8038° |
| revolutions per day: | 14.84986769 |
| mean anomaly at epoch: | 315.4125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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