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 66495U 26145.41159122 +.00000000 +00000-0 +81042-3 0 00004
2 66495 42.9996 277.3176 0000643 275.2638 84.8140 15.27595043 06
| Epoch (UTC): | 25 May 2026 09:52:41 |
| Eccentricity: | 0.0000643 |
| inclination: | 42.9996° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 277.3176° |
| argument of perigee: | 275.2638° |
| revolutions per day: | 15.27595043 |
| mean anomaly at epoch: | 84.8140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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