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 40044U 26088.18109361 +.00000000 +00000-0 +34988-3 0 00003
2 40044 97.7751 239.8315 0048033 342.1770 17.7758 14.84896245 09
| Epoch (UTC): | 29 March 2026 04:20:46 |
| Eccentricity: | 0.0048033 |
| inclination: | 97.7751° |
| perigee height: | 580 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 239.8315° |
| argument of perigee: | 342.1770° |
| revolutions per day: | 14.84896245 |
| mean anomaly at epoch: | 17.7758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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