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 30580U 26144.63706941 +.00000000 +00000-0 +24534-1 0 00001
2 30580 8.0494 111.7461 8373708 194.5882 97.3939 0.87844116 06
| Epoch (UTC): | 24 May 2026 15:17:22 |
| Eccentricity: | 0.8373708 |
| inclination: | 8.0494° |
| perigee height: | 1111 km |
| apogee height: | 78239 km |
| right ascension of ascending node: | 111.7461° |
| argument of perigee: | 194.5882° |
| revolutions per day: | 0.87844116 |
| mean anomaly at epoch: | 97.3939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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