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 44714U 26145.46515765 +.00000000 +00000-0 +82283-3 0 00006
2 44714 53.1533 177.2756 0002925 39.6871 320.4351 15.47077959 01
| Epoch (UTC): | 25 May 2026 11:09:49 |
| Eccentricity: | 0.0002925 |
| inclination: | 53.1533° |
| perigee height: | 423 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 177.2756° |
| argument of perigee: | 39.6871° |
| revolutions per day: | 15.47077959 |
| mean anomaly at epoch: | 320.4351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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