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 66951U 26145.32490053 +.00000000 +00000-0 +71936-3 0 00003
2 66951 53.1607 2.2204 0002161 93.6206 266.5044 15.34416275 02
| Epoch (UTC): | 25 May 2026 07:47:51 |
| Eccentricity: | 0.0002161 |
| inclination: | 53.1607° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 2.2204° |
| argument of perigee: | 93.6206° |
| revolutions per day: | 15.34416275 |
| mean anomaly at epoch: | 266.5044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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