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 66840U 26145.39676360 +.00000000 +00000-0 +25335-3 0 00006
2 66840 70.0006 141.1422 0003234 268.4489 91.6300 14.98336926 07
| Epoch (UTC): | 25 May 2026 09:31:20 |
| Eccentricity: | 0.0003234 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 141.1422° |
| argument of perigee: | 268.4489° |
| revolutions per day: | 14.98336926 |
| mean anomaly at epoch: | 91.6300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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