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 66697U 26145.45140284 +.00000000 +00000-0 +32228-3 0 00003
2 66697 97.4187 219.5690 0002925 69.5966 290.5583 15.20459269 08
| Epoch (UTC): | 25 May 2026 10:50:01 |
| Eccentricity: | 0.0002925 |
| inclination: | 97.4187° |
| perigee height: | 502 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.5690° |
| argument of perigee: | 69.5966° |
| revolutions per day: | 15.20459269 |
| mean anomaly at epoch: | 290.5583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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