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 66666U 26145.47124425 +.00000000 +00000-0 +11029-3 0 00006
2 66666 97.6548 220.0563 0006594 0.6857 359.4375 15.01078769 09
| Epoch (UTC): | 25 May 2026 11:18:35 |
| Eccentricity: | 0.0006594 |
| inclination: | 97.6548° |
| perigee height: | 559 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 220.0563° |
| argument of perigee: | 0.6857° |
| revolutions per day: | 15.01078769 |
| mean anomaly at epoch: | 359.4375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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