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 64776U 26145.53472502 +.00000000 +00000-0 +26360-3 0 00009
2 64776 53.1623 245.3423 0000189 191.5713 168.5286 15.34388980 05
| Epoch (UTC): | 25 May 2026 12:50:00 |
| Eccentricity: | 0.0000189 |
| inclination: | 53.1623° |
| perigee height: | 463 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 245.3423° |
| argument of perigee: | 191.5713° |
| revolutions per day: | 15.34388980 |
| mean anomaly at epoch: | 168.5286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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