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 61912U 26145.52536397 +.00000000 +00000-0 +48070-3 0 00002
2 61912 43.0012 207.7679 0001352 277.0187 83.0511 15.27580364 01
| Epoch (UTC): | 25 May 2026 12:36:31 |
| Eccentricity: | 0.0001352 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.7679° |
| argument of perigee: | 277.0187° |
| revolutions per day: | 15.27580364 |
| mean anomaly at epoch: | 83.0511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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