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 61880U 26145.53729507 +.00000000 +00000-0 +12854-4 0 00006
2 61880 53.1579 337.4871 0000861 59.1570 300.9532 15.69708858 09
| Epoch (UTC): | 25 May 2026 12:53:42 |
| Eccentricity: | 0.0000861 |
| inclination: | 53.1579° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 337.4871° |
| argument of perigee: | 59.1570° |
| revolutions per day: | 15.69708858 |
| mean anomaly at epoch: | 300.9532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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