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 61942U 26145.28633566 +.00000000 +00000-0 +22726-2 0 00003
2 61942 53.1567 354.0090 0000871 61.3592 298.7513 15.69796024 08
| Epoch (UTC): | 25 May 2026 06:52:19 |
| Eccentricity: | 0.0000871 |
| inclination: | 53.1567° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 354.0090° |
| argument of perigee: | 61.3592° |
| revolutions per day: | 15.69796024 |
| mean anomaly at epoch: | 298.7513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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