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 66754U 26145.15997034 +.00000000 +00000-0 +15146-3 0 00007
2 66754 97.4207 219.0840 0004691 72.9846 287.1902 15.18237141 01
| Epoch (UTC): | 25 May 2026 03:50:21 |
| Eccentricity: | 0.0004691 |
| inclination: | 97.4207° |
| perigee height: | 508 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 219.0840° |
| argument of perigee: | 72.9846° |
| revolutions per day: | 15.18237141 |
| mean anomaly at epoch: | 287.1902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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