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 48318U 26145.18722654 +.00000000 +00000-0 +14275-4 0 00003
2 48318 53.1597 106.0704 0001104 92.6510 267.4617 15.31701283 07
| Epoch (UTC): | 25 May 2026 04:29:36 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 106.0704° |
| argument of perigee: | 92.6510° |
| revolutions per day: | 15.31701283 |
| mean anomaly at epoch: | 267.4617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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