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 64808U 26144.65157481 +.00000000 +00000-0 +23524-3 0 00002
2 64808 70.0006 302.9867 0002932 268.2299 91.8525 14.98336068 08
| Epoch (UTC): | 24 May 2026 15:38:16 |
| Eccentricity: | 0.0002932 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 302.9867° |
| argument of perigee: | 268.2299° |
| revolutions per day: | 14.98336068 |
| mean anomaly at epoch: | 91.8525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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