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 39444U 26072.35704843 +.00000000 +00000-0 +51353-3 0 00008
2 39444 97.8186 41.9580 0037754 166.4701 193.7548 15.07980612 09
| Epoch (UTC): | 13 March 2026 08:34:08 |
| Eccentricity: | 0.0037754 |
| inclination: | 97.8186° |
| perigee height: | 516 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 41.9580° |
| argument of perigee: | 166.4701° |
| revolutions per day: | 15.07980612 |
| mean anomaly at epoch: | 193.7548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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