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 66301U 26145.32841182 +.00000000 +00000-0 +24921-3 0 00007
2 66301 45.4014 253.9496 0006163 261.1984 98.8200 15.08860800 04
| Epoch (UTC): | 25 May 2026 07:52:54 |
| Eccentricity: | 0.0006163 |
| inclination: | 45.4014° |
| perigee height: | 535 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 253.9496° |
| argument of perigee: | 261.1984° |
| revolutions per day: | 15.08860800 |
| mean anomaly at epoch: | 98.8200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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