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 66748U 26145.17801985 +.00000000 +00000-0 +87500-3 0 00004
2 66748 97.4205 219.9688 0003343 84.7183 275.4437 15.25556084 00
| Epoch (UTC): | 25 May 2026 04:16:20 |
| Eccentricity: | 0.0003343 |
| inclination: | 97.4205° |
| perigee height: | 487 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 219.9688° |
| argument of perigee: | 84.7183° |
| revolutions per day: | 15.25556084 |
| mean anomaly at epoch: | 275.4437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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