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 66734U 26145.45092446 +.00000000 +00000-0 +25973-3 0 00000
2 66734 97.4172 219.2297 0005488 99.2720 260.9136 15.19331517 07
| Epoch (UTC): | 25 May 2026 10:49:19 |
| Eccentricity: | 0.0005488 |
| inclination: | 97.4172° |
| perigee height: | 504 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 219.2297° |
| argument of perigee: | 99.2720° |
| revolutions per day: | 15.19331517 |
| mean anomaly at epoch: | 260.9136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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