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 64851U 26145.30799244 +.00000000 +00000-0 +28718-3 0 00002
2 64851 97.4509 0.6045 0002591 83.2315 276.9207 15.05653106 09
| Epoch (UTC): | 25 May 2026 07:23:30 |
| Eccentricity: | 0.0002591 |
| inclination: | 97.4509° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.6045° |
| argument of perigee: | 83.2315° |
| revolutions per day: | 15.05653106 |
| mean anomaly at epoch: | 276.9207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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