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 64551U 26145.28039551 +.00000000 +00000-0 +30025-3 0 00008
2 64551 97.4588 261.1221 0001325 57.2008 302.9357 15.24571003 09
| Epoch (UTC): | 25 May 2026 06:43:46 |
| Eccentricity: | 0.0001325 |
| inclination: | 97.4588° |
| perigee height: | 491 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 261.1221° |
| argument of perigee: | 57.2008° |
| revolutions per day: | 15.24571003 |
| mean anomaly at epoch: | 302.9357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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