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 61903U 26101.53455264 +.00000000 +00000-0 +36043-3 0 00005
2 61903 97.4128 178.6834 0008635 272.3366 87.6885 15.29019100 00
| Epoch (UTC): | 11 April 2026 12:49:45 |
| Eccentricity: | 0.0008635 |
| inclination: | 97.4128° |
| perigee height: | 473 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 178.6834° |
| argument of perigee: | 272.3366° |
| revolutions per day: | 15.29019100 |
| mean anomaly at epoch: | 87.6885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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