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 48371U 26145.28501867 +.00000000 +00000-0 +61764-4 0 00009
2 48371 53.1612 351.6475 0002462 79.8778 280.2502 15.31707447 02
| Epoch (UTC): | 25 May 2026 06:50:25 |
| Eccentricity: | 0.0002462 |
| inclination: | 53.1612° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 351.6475° |
| argument of perigee: | 79.8778° |
| revolutions per day: | 15.31707447 |
| mean anomaly at epoch: | 280.2502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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