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 53064U 26145.46623814 +.00000000 +00000-0 +66071-3 0 00006
2 53064 97.4477 326.5118 0001404 132.7610 227.3736 15.05610315 00
| Epoch (UTC): | 25 May 2026 11:11:22 |
| Eccentricity: | 0.0001404 |
| inclination: | 97.4477° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.5118° |
| argument of perigee: | 132.7610° |
| revolutions per day: | 15.05610315 |
| mean anomaly at epoch: | 227.3736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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