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 08860U 26053.04956538 +.00000000 +00000-0 +11276-3 0 00001
2 08860 99.9177 263.3376 0041194 291.1783 222.8706 13.68272521 00
| Epoch (UTC): | 22 February 2026 01:11:22 |
| Eccentricity: | 0.0041194 |
| inclination: | 99.9177° |
| perigee height: | 975 km |
| apogee height: | 1036 km |
| right ascension of ascending node: | 263.3376° |
| argument of perigee: | 291.1783° |
| revolutions per day: | 13.68272521 |
| mean anomaly at epoch: | 222.8706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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