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 64252U 26145.54653286 +.00000000 +00000-0 +53376-3 0 00006
2 64252 42.9991 232.9948 0000402 307.3646 52.7169 15.27603411 07
| Epoch (UTC): | 25 May 2026 13:07:00 |
| Eccentricity: | 0.0000402 |
| inclination: | 42.9991° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 232.9948° |
| argument of perigee: | 307.3646° |
| revolutions per day: | 15.27603411 |
| mean anomaly at epoch: | 52.7169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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