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 44771U 26145.37851303 +.00000000 +00000-0 +47295-3 0 00004
2 44771 53.0428 187.6541 0006812 341.1682 18.9083 15.72388679 06
| Epoch (UTC): | 25 May 2026 09:05:03 |
| Eccentricity: | 0.0006812 |
| inclination: | 53.0428° |
| perigee height: | 347 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 187.6541° |
| argument of perigee: | 341.1682° |
| revolutions per day: | 15.72388679 |
| mean anomaly at epoch: | 18.9083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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