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 26100.17593189 +.00000000 +00000-0 +14756-4 0 00005
2 08519 81.2463 190.7954 0013762 153.4250 206.7630 14.11379419 07
| Epoch (UTC): | 10 April 2026 04:13:20 |
| Eccentricity: | 0.0013762 |
| inclination: | 81.2463° |
| perigee height: | 845 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 190.7954° |
| argument of perigee: | 153.4250° |
| revolutions per day: | 14.11379419 |
| mean anomaly at epoch: | 206.7630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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