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 66678U 26145.46484211 +.00000000 +00000-0 +30952-3 0 00006
2 66678 97.4217 219.3224 0007383 83.5432 276.6644 15.19396553 06
| Epoch (UTC): | 25 May 2026 11:09:22 |
| Eccentricity: | 0.0007383 |
| inclination: | 97.4217° |
| perigee height: | 503 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.3224° |
| argument of perigee: | 83.5432° |
| revolutions per day: | 15.19396553 |
| mean anomaly at epoch: | 276.6644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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