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 35868U 26025.45991631 +.00000000 +00000-0 +20457-3 0 00007
2 35868 98.6994 348.9008 0003642 343.7949 16.3113 14.24159297 02
| Epoch (UTC): | 25 January 2026 11:02:16 |
| Eccentricity: | 0.0003642 |
| inclination: | 98.6994° |
| perigee height: | 809 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 348.9008° |
| argument of perigee: | 343.7949° |
| revolutions per day: | 14.24159297 |
| mean anomaly at epoch: | 16.3113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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