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 07530U 26145.50123808 +.00000000 +00000-0 +95166-4 0 00004
2 07530 101.9908 158.5111 0012321 172.6684 342.7297 12.53697657 05
| Epoch (UTC): | 25 May 2026 12:01:46 |
| Eccentricity: | 0.0012321 |
| inclination: | 101.9908° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 158.5111° |
| argument of perigee: | 172.6684° |
| revolutions per day: | 12.53697657 |
| mean anomaly at epoch: | 342.7297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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