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 66391U 26145.50141186 +.00000000 +00000-0 +38949-3 0 00008
2 66391 53.1579 223.0778 0001107 101.3685 258.7440 15.30204265 07
| Epoch (UTC): | 25 May 2026 12:02:01 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.1579° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.0778° |
| argument of perigee: | 101.3685° |
| revolutions per day: | 15.30204265 |
| mean anomaly at epoch: | 258.7440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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