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 61879U 26145.54220473 +.00000000 +00000-0 +30400-5 0 00001
2 61879 53.1591 337.5186 0001222 116.4935 243.6209 15.69717502 05
| Epoch (UTC): | 25 May 2026 13:00:46 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 337.5186° |
| argument of perigee: | 116.4935° |
| revolutions per day: | 15.69717502 |
| mean anomaly at epoch: | 243.6209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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