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 61977U 26145.35986417 +.00000000 +00000-0 +47256-3 0 00001
2 61977 43.0015 106.9994 0001713 270.7919 89.2737 15.27593130 02
| Epoch (UTC): | 25 May 2026 08:38:12 |
| Eccentricity: | 0.0001713 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.9994° |
| argument of perigee: | 270.7919° |
| revolutions per day: | 15.27593130 |
| mean anomaly at epoch: | 89.2737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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