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 66704U 26145.14578520 +.00000000 +00000-0 +23099-3 0 00002
2 66704 97.4182 219.1999 0003215 66.3228 293.8345 15.20254492 02
| Epoch (UTC): | 25 May 2026 03:29:55 |
| Eccentricity: | 0.0003215 |
| inclination: | 97.4182° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.1999° |
| argument of perigee: | 66.3228° |
| revolutions per day: | 15.20254492 |
| mean anomaly at epoch: | 293.8345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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