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 66297U 26145.53632157 +.00000000 +00000-0 +16450-3 0 00002
2 66297 45.4063 239.9829 0011593 274.5268 85.4295 15.22493991 07
| Epoch (UTC): | 25 May 2026 12:52:18 |
| Eccentricity: | 0.0011593 |
| inclination: | 45.4063° |
| perigee height: | 490 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 239.9829° |
| argument of perigee: | 274.5268° |
| revolutions per day: | 15.22493991 |
| mean anomaly at epoch: | 85.4295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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