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 25442U 26087.28312830 +.00000000 +00000-0 +71219-3 0 00003
2 25442 81.7524 41.6469 0201562 159.2292 201.7253 14.62199537 09
| Epoch (UTC): | 28 March 2026 06:47:42 |
| Eccentricity: | 0.0201562 |
| inclination: | 81.7524° |
| perigee height: | 544 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 41.6469° |
| argument of perigee: | 159.2292° |
| revolutions per day: | 14.62199537 |
| mean anomaly at epoch: | 201.7253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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