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 10702U 26099.82913306 +.00000000 +00000-0 +11301-3 0 00000
2 10702 99.0620 55.9846 0014332 336.5479 87.6599 13.96994065 01
| Epoch (UTC): | 09 April 2026 19:53:57 |
| Eccentricity: | 0.0014332 |
| inclination: | 99.0620° |
| perigee height: | 894 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 55.9846° |
| argument of perigee: | 336.5479° |
| revolutions per day: | 13.96994065 |
| mean anomaly at epoch: | 87.6599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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