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 66930U 26145.33960838 +.00000000 +00000-0 +31555-3 0 00007
2 66930 53.1606 2.3142 0000830 131.8156 228.2917 15.34410888 08
| Epoch (UTC): | 25 May 2026 08:09:02 |
| Eccentricity: | 0.0000830 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 2.3142° |
| argument of perigee: | 131.8156° |
| revolutions per day: | 15.34410888 |
| mean anomaly at epoch: | 228.2917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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