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 35951U 26032.50388934 +.00000000 +00000-0 +16826-3 0 00005
2 35951 98.8901 13.6695 0010052 278.2489 81.7544 14.14810071 04
| Epoch (UTC): | 01 February 2026 12:05:36 |
| Eccentricity: | 0.0010052 |
| inclination: | 98.8901° |
| perigee height: | 836 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 13.6695° |
| argument of perigee: | 278.2489° |
| revolutions per day: | 14.14810071 |
| mean anomaly at epoch: | 81.7544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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