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 64800U 26145.43182309 +.00000000 +00000-0 +31880-3 0 00002
2 64800 70.0004 300.8961 0003037 263.5605 96.5208 14.98337152 01
| Epoch (UTC): | 25 May 2026 10:21:49 |
| Eccentricity: | 0.0003037 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8961° |
| argument of perigee: | 263.5605° |
| revolutions per day: | 14.98337152 |
| mean anomaly at epoch: | 96.5208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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