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 66700U 26145.10482933 +.00000000 +00000-0 +21657-3 0 00004
2 66700 97.4221 219.3477 0002622 73.7670 286.3854 15.20898012 03
| Epoch (UTC): | 25 May 2026 02:30:57 |
| Eccentricity: | 0.0002622 |
| inclination: | 97.4221° |
| perigee height: | 501 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.3477° |
| argument of perigee: | 73.7670° |
| revolutions per day: | 15.20898012 |
| mean anomaly at epoch: | 286.3854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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