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 64957U 26145.58288571 +.00000000 +00000-0 +14412-3 0 00001
2 64957 86.4944 290.1232 0001992 92.3765 267.7597 13.24405978 06
| Epoch (UTC): | 25 May 2026 13:59:21 |
| Eccentricity: | 0.0001992 |
| inclination: | 86.4944° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 290.1232° |
| argument of perigee: | 92.3765° |
| revolutions per day: | 13.24405978 |
| mean anomaly at epoch: | 267.7597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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