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 08520U 26088.12668867 +.00000000 +00000-0 +68230-4 0 00009
2 08520 81.2870 307.0969 0027422 278.5397 81.2666 14.09431129 08
| Epoch (UTC): | 29 March 2026 03:02:25 |
| Eccentricity: | 0.0027422 |
| inclination: | 81.2870° |
| perigee height: | 841 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 307.0969° |
| argument of perigee: | 278.5397° |
| revolutions per day: | 14.09431129 |
| mean anomaly at epoch: | 81.2666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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