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 61251U 26145.41979361 +.00000000 +00000-0 +19076-4 0 00003
2 61251 53.1611 38.3201 0001241 70.5587 289.5564 15.69704248 06
| Epoch (UTC): | 25 May 2026 10:04:30 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.1611° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 38.3201° |
| argument of perigee: | 70.5587° |
| revolutions per day: | 15.69704248 |
| mean anomaly at epoch: | 289.5564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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