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 20508U 26053.70912994 +.00000000 +00000-0 +66570-4 0 00003
2 20508 82.9600 158.5853 0044759 40.4994 82.0096 13.74546427 04
| Epoch (UTC): | 22 February 2026 17:01:08 |
| Eccentricity: | 0.0044759 |
| inclination: | 82.9600° |
| perigee height: | 950 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 158.5853° |
| argument of perigee: | 40.4994° |
| revolutions per day: | 13.74546427 |
| mean anomaly at epoch: | 82.0096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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