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 66992U 25291A 26002.73478675 0.00000000 00000-0 00000-0 0 01
2 66992 63.4387 211.9441 0128409 181.6333 178.3667 13.40956314 00
| Epoch (UTC): | 02 January 2026 17:38:05 |
| Eccentricity: | 0.0128409 |
| inclination: | 63.4387° |
| perigee height: | 1009 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 211.9441° |
| argument of perigee: | 181.6333° |
| revolutions per day: | 13.40956314 |
| mean anomaly at epoch: | 178.3667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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