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 61207U 26145.43442822 +.00000000 +00000-0 +19941-4 0 00004
2 61207 53.1597 157.8440 0001212 99.2174 260.8981 15.69708413 03
| Epoch (UTC): | 25 May 2026 10:25:34 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 157.8440° |
| argument of perigee: | 99.2174° |
| revolutions per day: | 15.69708413 |
| mean anomaly at epoch: | 260.8981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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