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 07531U 26121.81605030 +.00000000 +00000-0 +89575-4 0 00002
2 07531 101.9957 133.7027 0011028 229.1717 304.1429 12.53529156 06
| Epoch (UTC): | 01 May 2026 19:35:06 |
| Eccentricity: | 0.0011028 |
| inclination: | 101.9957° |
| perigee height: | 1441 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 133.7027° |
| argument of perigee: | 229.1717° |
| revolutions per day: | 12.53529156 |
| mean anomaly at epoch: | 304.1429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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