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 66714U 26145.61955477 +.00000000 +00000-0 +59932-3 0 00000
2 66714 97.4206 219.8604 0004490 99.6694 260.5050 15.21907394 03
| Epoch (UTC): | 25 May 2026 14:52:09 |
| Eccentricity: | 0.0004490 |
| inclination: | 97.4206° |
| perigee height: | 497 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 219.8604° |
| argument of perigee: | 99.6694° |
| revolutions per day: | 15.21907394 |
| mean anomaly at epoch: | 260.5050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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