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 50200U 26145.58628324 +.00000000 +00000-0 +17799-4 0 00003
2 50200 53.2140 253.8783 0001556 92.4777 267.6393 15.08837442 01
| Epoch (UTC): | 25 May 2026 14:04:14 |
| Eccentricity: | 0.0001556 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 253.8783° |
| argument of perigee: | 92.4777° |
| revolutions per day: | 15.08837442 |
| mean anomaly at epoch: | 267.6393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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