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 48124U 26145.34020784 +.00000000 +00000-0 +93806-5 0 00009
2 48124 53.1585 158.4582 0001254 89.4672 270.6474 15.31696180 09
| Epoch (UTC): | 25 May 2026 08:09:53 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 158.4582° |
| argument of perigee: | 89.4672° |
| revolutions per day: | 15.31696180 |
| mean anomaly at epoch: | 270.6474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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