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 10874U 26067.92941108 +.00000000 +00000-0 +32250-2 0 00002
2 10874 101.9986 219.7063 0080135 142.0048 345.7081 13.16709650 06
| Epoch (UTC): | 08 March 2026 22:18:21 |
| Eccentricity: | 0.0080135 |
| inclination: | 101.9986° |
| perigee height: | 1137 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 219.7063° |
| argument of perigee: | 142.0048° |
| revolutions per day: | 13.16709650 |
| mean anomaly at epoch: | 345.7081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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