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 64150U 26145.12924279 +.00000000 +00000-0 -98828-3 0 00002
2 64150 97.4514 196.5457 0001470 184.5936 175.5278 15.05605416 01
| Epoch (UTC): | 25 May 2026 03:06:06 |
| Eccentricity: | 0.0001470 |
| inclination: | 97.4514° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.5457° |
| argument of perigee: | 184.5936° |
| revolutions per day: | 15.05605416 |
| mean anomaly at epoch: | 175.5278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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