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 66705U 26145.45738178 +.00000000 +00000-0 +25094-3 0 00001
2 66705 97.4178 219.5374 0002559 75.0180 285.1339 15.20511166 04
| Epoch (UTC): | 25 May 2026 10:58:37 |
| Eccentricity: | 0.0002559 |
| inclination: | 97.4178° |
| perigee height: | 503 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.5374° |
| argument of perigee: | 75.0180° |
| revolutions per day: | 15.20511166 |
| mean anomaly at epoch: | 285.1339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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