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 64367U 26145.38909641 +.00000000 +00000-0 +23403-3 0 00002
2 64367 70.0005 200.9452 0003969 263.8476 96.2231 14.98340134 05
| Epoch (UTC): | 25 May 2026 09:20:17 |
| Eccentricity: | 0.0003969 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.9452° |
| argument of perigee: | 263.8476° |
| revolutions per day: | 14.98340134 |
| mean anomaly at epoch: | 96.2231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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