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 66723U 26145.62443856 +.00000000 +00000-0 +27310-3 0 00009
2 66723 97.4220 219.8741 0003269 49.5268 310.6252 15.20870970 04
| Epoch (UTC): | 25 May 2026 14:59:11 |
| Eccentricity: | 0.0003269 |
| inclination: | 97.4220° |
| perigee height: | 501 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.8741° |
| argument of perigee: | 49.5268° |
| revolutions per day: | 15.20870970 |
| mean anomaly at epoch: | 310.6252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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