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 66687U 26145.15010022 +.00000000 +00000-0 +46242-3 0 00006
2 66687 97.4262 219.1502 0005393 217.0084 143.0780 15.20463363 03
| Epoch (UTC): | 25 May 2026 03:36:08 |
| Eccentricity: | 0.0005393 |
| inclination: | 97.4262° |
| perigee height: | 501 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 219.1502° |
| argument of perigee: | 217.0084° |
| revolutions per day: | 15.20463363 |
| mean anomaly at epoch: | 143.0780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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