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 10962U 26068.52528161 +.00000000 +00000-0 +12197-3 0 00006
2 10962 74.0762 90.3886 0026139 252.7760 107.0535 14.42843857 07
| Epoch (UTC): | 09 March 2026 12:36:24 |
| Eccentricity: | 0.0026139 |
| inclination: | 74.0762° |
| perigee height: | 730 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 90.3886° |
| argument of perigee: | 252.7760° |
| revolutions per day: | 14.42843857 |
| mean anomaly at epoch: | 107.0535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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