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 44340U 26145.31027352 +.00000000 +00000-0 +74920-3 0 00004
2 44340 24.0004 6.7261 0007628 312.9920 46.9937 14.74331843 04
| Epoch (UTC): | 25 May 2026 07:26:47 |
| Eccentricity: | 0.0007628 |
| inclination: | 24.0004° |
| perigee height: | 642 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 6.7261° |
| argument of perigee: | 312.9920° |
| revolutions per day: | 14.74331843 |
| mean anomaly at epoch: | 46.9937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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