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 48093U 26145.41478212 +.00000000 +00000-0 +57483-4 0 00005
2 48093 53.1613 158.0727 0001204 96.2170 263.8969 15.31703746 07
| Epoch (UTC): | 25 May 2026 09:57:17 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 158.0727° |
| argument of perigee: | 96.2170° |
| revolutions per day: | 15.31703746 |
| mean anomaly at epoch: | 263.8969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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