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 44744U 26145.49642654 +.00000000 +00000-0 +11245-2 0 00009
2 44744 53.0576 220.3961 0003095 3.9451 356.1571 15.27563900 09
| Epoch (UTC): | 25 May 2026 11:54:51 |
| Eccentricity: | 0.0003095 |
| inclination: | 53.0576° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 220.3961° |
| argument of perigee: | 3.9451° |
| revolutions per day: | 15.27563900 |
| mean anomaly at epoch: | 356.1571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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