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 66914U 26145.20425477 +.00000000 +00000-0 +87885-4 0 00008
2 66914 80.3971 313.2183 0010730 299.6915 60.3177 13.97316636 08
| Epoch (UTC): | 25 May 2026 04:54:07 |
| Eccentricity: | 0.0010730 |
| inclination: | 80.3971° |
| perigee height: | 895 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 313.2183° |
| argument of perigee: | 299.6915° |
| revolutions per day: | 13.97316636 |
| mean anomaly at epoch: | 60.3177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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