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 61902U 26145.64939750 +.00000000 +00000-0 +36038-3 0 00005
2 61902 97.4146 216.6900 0011905 242.2382 117.7642 15.11773972 05
| Epoch (UTC): | 25 May 2026 15:35:07 |
| Eccentricity: | 0.0011905 |
| inclination: | 97.4146° |
| perigee height: | 523 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 216.6900° |
| argument of perigee: | 242.2382° |
| revolutions per day: | 15.11773972 |
| mean anomaly at epoch: | 117.7642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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