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 66862U 26145.63688574 +.00000000 +00000-0 +42535-3 0 00008
2 66862 43.0010 268.9131 0000749 259.6231 100.4536 15.27588027 00
| Epoch (UTC): | 25 May 2026 15:17:06 |
| Eccentricity: | 0.0000749 |
| inclination: | 43.0010° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 268.9131° |
| argument of perigee: | 259.6231° |
| revolutions per day: | 15.27588027 |
| mean anomaly at epoch: | 100.4536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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