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 66677U 26145.14529073 +.00000000 +00000-0 +47598-3 0 00000
2 66677 97.4184 219.3573 0006864 97.9917 262.2098 15.22205517 02
| Epoch (UTC): | 25 May 2026 03:29:13 |
| Eccentricity: | 0.0006864 |
| inclination: | 97.4184° |
| perigee height: | 494 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 219.3573° |
| argument of perigee: | 97.9917° |
| revolutions per day: | 15.22205517 |
| mean anomaly at epoch: | 262.2098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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