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 66880U 26144.95817398 +.00000000 +00000-0 +47759-3 0 00003
2 66880 53.1599 29.7346 0000853 86.4118 273.6980 15.30208094 04
| Epoch (UTC): | 24 May 2026 22:59:46 |
| Eccentricity: | 0.0000853 |
| inclination: | 53.1599° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.7346° |
| argument of perigee: | 86.4118° |
| revolutions per day: | 15.30208094 |
| mean anomaly at epoch: | 273.6980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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