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 08820U 26145.37143932 +.00000000 +00000-0 +00000-0 0 00001
2 08820 109.8030 171.5295 0044678 307.1510 58.2151 6.38664707 06
| Epoch (UTC): | 25 May 2026 08:54:52 |
| Eccentricity: | 0.0044678 |
| inclination: | 109.8030° |
| perigee height: | 5838 km |
| apogee height: | 5948 km |
| right ascension of ascending node: | 171.5295° |
| argument of perigee: | 307.1510° |
| revolutions per day: | 6.38664707 |
| mean anomaly at epoch: | 58.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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