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 64878U 26145.50059402 +.00000000 +00000-0 +21661-3 0 00008
2 64878 97.4548 112.7074 0008499 265.2001 94.8267 15.25172783 07
| Epoch (UTC): | 25 May 2026 12:00:51 |
| Eccentricity: | 0.0008499 |
| inclination: | 97.4548° |
| perigee height: | 484 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 112.7074° |
| argument of perigee: | 265.2001° |
| revolutions per day: | 15.25172783 |
| mean anomaly at epoch: | 94.8267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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