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 44961U 26145.58335647 +.00000000 +00000-0 -36589-2 0 00000
2 44961 53.0453 277.0619 0001341 71.9718 160.8958 15.66317628 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.0453° |
| perigee height: | 369 km |
| apogee height: | 370 km |
| right ascension of ascending node: | 277.0619° |
| argument of perigee: | 71.9718° |
| revolutions per day: | 15.66317628 |
| mean anomaly at epoch: | 160.8958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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