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 66696U 26145.46230985 +.00000000 +00000-0 +34274-3 0 00004
2 66696 97.4189 219.4048 0005378 93.7452 266.4398 15.20064505 00
| Epoch (UTC): | 25 May 2026 11:05:43 |
| Eccentricity: | 0.0005378 |
| inclination: | 97.4189° |
| perigee height: | 502 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.4048° |
| argument of perigee: | 93.7452° |
| revolutions per day: | 15.20064505 |
| mean anomaly at epoch: | 266.4398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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