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 53828U 26145.20309713 +.00000000 +00000-0 +44241-4 0 00001
2 53828 53.2141 320.5441 0001297 85.4233 274.6908 15.08838243 05
| Epoch (UTC): | 25 May 2026 04:52:27 |
| Eccentricity: | 0.0001297 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 320.5441° |
| argument of perigee: | 85.4233° |
| revolutions per day: | 15.08838243 |
| mean anomaly at epoch: | 274.6908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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