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 50165U 26144.60188660 +.00000000 +00000-0 +34364-4 0 00006
2 50165 53.2155 278.3360 0001265 91.4223 268.6914 15.08837804 04
| Epoch (UTC): | 24 May 2026 14:26:43 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 278.3360° |
| argument of perigee: | 91.4223° |
| revolutions per day: | 15.08837804 |
| mean anomaly at epoch: | 268.6914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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