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 66300U 26145.35758157 +.00000000 +00000-0 +27083-3 0 00000
2 66300 45.4043 254.2173 0006513 266.4769 93.5368 15.08768821 06
| Epoch (UTC): | 25 May 2026 08:34:55 |
| Eccentricity: | 0.0006513 |
| inclination: | 45.4043° |
| perigee height: | 535 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 254.2173° |
| argument of perigee: | 266.4769° |
| revolutions per day: | 15.08768821 |
| mean anomaly at epoch: | 93.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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