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 58022U 26145.12995027 +.00000000 +00000-0 +34383-3 0 00007
2 58022 97.5373 214.9565 0006902 329.3162 30.7663 15.10562027 02
| Epoch (UTC): | 25 May 2026 03:07:07 |
| Eccentricity: | 0.0006902 |
| inclination: | 97.5373° |
| perigee height: | 530 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 214.9565° |
| argument of perigee: | 329.3162° |
| revolutions per day: | 15.10562027 |
| mean anomaly at epoch: | 30.7663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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