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 10953U 26031.25901413 +.00000000 +00000-0 +00000-0 0 00008
2 10953 7.2107 300.2673 0003340 340.9422 206.3297 0.99357551 05
| Epoch (UTC): | 31 January 2026 06:12:58 |
| Eccentricity: | 0.0003340 |
| inclination: | 7.2107° |
| perigee height: | 36031 km |
| apogee height: | 36059 km |
| right ascension of ascending node: | 300.2673° |
| argument of perigee: | 340.9422° |
| revolutions per day: | 0.99357551 |
| mean anomaly at epoch: | 206.3297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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