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 66733U 26145.17361412 +.00000000 +00000-0 +27538-3 0 00009
2 66733 97.4236 219.1390 0005951 94.3753 265.8162 15.19517063 02
| Epoch (UTC): | 25 May 2026 04:10:00 |
| Eccentricity: | 0.0005951 |
| inclination: | 97.4236° |
| perigee height: | 503 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.1390° |
| argument of perigee: | 94.3753° |
| revolutions per day: | 15.19517063 |
| mean anomaly at epoch: | 265.8162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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