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 66709U 26145.17541317 +.00000000 +00000-0 +24526-3 0 00000
2 66709 97.4233 219.2801 0004532 68.7938 291.3781 15.19980266 04
| Epoch (UTC): | 25 May 2026 04:12:35 |
| Eccentricity: | 0.0004532 |
| inclination: | 97.4233° |
| perigee height: | 503 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.2801° |
| argument of perigee: | 68.7938° |
| revolutions per day: | 15.19980266 |
| mean anomaly at epoch: | 291.3781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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