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 51461U 26145.40964772 +.00000000 +00000-0 +41812-4 0 00007
2 51461 53.2128 294.7111 0001300 88.9665 271.1476 15.08838714 04
| Epoch (UTC): | 25 May 2026 09:49:53 |
| Eccentricity: | 0.0001300 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.7111° |
| argument of perigee: | 88.9665° |
| revolutions per day: | 15.08838714 |
| mean anomaly at epoch: | 271.1476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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