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 66997U 26145.10978275 +.00000000 +00000-0 +21641-3 0 00004
2 66997 97.6330 221.1144 0016023 83.3062 276.9988 15.06190958 09
| Epoch (UTC): | 25 May 2026 02:38:05 |
| Eccentricity: | 0.0016023 |
| inclination: | 97.6330° |
| perigee height: | 537 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 221.1144° |
| argument of perigee: | 83.3062° |
| revolutions per day: | 15.06190958 |
| mean anomaly at epoch: | 276.9988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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