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 08519U 26088.05333434 +.00000000 +00000-0 +76810-4 0 00001
2 08519 81.2461 202.6157 0013364 185.0255 175.0785 14.11376777 00
| Epoch (UTC): | 29 March 2026 01:16:48 |
| Eccentricity: | 0.0013364 |
| inclination: | 81.2461° |
| perigee height: | 845 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 202.6157° |
| argument of perigee: | 185.0255° |
| revolutions per day: | 14.11376777 |
| mean anomaly at epoch: | 175.0785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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