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 48069U 26145.50863676 +.00000000 +00000-0 -15654-3 0 00004
2 48069 87.8946 324.7401 0001480 100.8063 259.3232 13.13468129 07
| Epoch (UTC): | 25 May 2026 12:12:26 |
| Eccentricity: | 0.0001480 |
| inclination: | 87.8946° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7401° |
| argument of perigee: | 100.8063° |
| revolutions per day: | 13.13468129 |
| mean anomaly at epoch: | 259.3232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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