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 66628U 26145.27817454 +.00000000 +00000-0 +97183-3 0 00008
2 66628 53.1580 142.7040 0001049 80.9257 279.1865 15.34419250 07
| Epoch (UTC): | 25 May 2026 06:40:34 |
| Eccentricity: | 0.0001049 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 142.7040° |
| argument of perigee: | 80.9257° |
| revolutions per day: | 15.34419250 |
| mean anomaly at epoch: | 279.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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