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 48467U 26145.42829522 +.00000000 +00000-0 +26287-4 0 00003
2 48467 53.1561 194.0778 0001277 80.3508 279.7637 15.31705551 03
| Epoch (UTC): | 25 May 2026 10:16:44 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1561° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.0778° |
| argument of perigee: | 80.3508° |
| revolutions per day: | 15.31705551 |
| mean anomaly at epoch: | 279.7637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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