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 61882U 26144.82713419 +.00000000 +00000-0 +68446-5 0 00003
2 61882 53.1585 340.8734 0000804 51.7996 308.3094 15.69696712 01
| Epoch (UTC): | 24 May 2026 19:51:04 |
| Eccentricity: | 0.0000804 |
| inclination: | 53.1585° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 340.8734° |
| argument of perigee: | 51.7996° |
| revolutions per day: | 15.69696712 |
| mean anomaly at epoch: | 308.3094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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