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 64880U 26145.62783075 +.00000000 +00000-0 +35031-3 0 00000
2 64880 97.4537 114.2315 0005528 252.0218 108.0420 15.30213826 06
| Epoch (UTC): | 25 May 2026 15:04:04 |
| Eccentricity: | 0.0005528 |
| inclination: | 97.4537° |
| perigee height: | 471 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 114.2315° |
| argument of perigee: | 252.0218° |
| revolutions per day: | 15.30213826 |
| mean anomaly at epoch: | 108.0420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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