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 48043U 26145.48833285 +.00000000 +00000-0 +89631-3 0 00001
2 48043 87.8942 324.7414 0001829 87.1766 272.9572 13.13468755 06
| Epoch (UTC): | 25 May 2026 11:43:11 |
| Eccentricity: | 0.0001829 |
| inclination: | 87.8942° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7414° |
| argument of perigee: | 87.1766° |
| revolutions per day: | 13.13468755 |
| mean anomaly at epoch: | 272.9572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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