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 39643U 26088.10036584 +.00000000 +00000-0 +19426-3 0 00004
2 39643 65.0096 228.1402 0016193 281.0588 78.8677 14.34660475 07
| Epoch (UTC): | 29 March 2026 02:24:31 |
| Eccentricity: | 0.0016193 |
| inclination: | 65.0096° |
| perigee height: | 765 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 228.1402° |
| argument of perigee: | 281.0588° |
| revolutions per day: | 14.34660475 |
| mean anomaly at epoch: | 78.8677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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