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 66984U 26145.18834174 +.00000000 +00000-0 +57427-3 0 00008
2 66984 43.0022 311.7081 0002922 269.3964 90.6553 15.27587363 06
| Epoch (UTC): | 25 May 2026 04:31:12 |
| Eccentricity: | 0.0002922 |
| inclination: | 43.0022° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 311.7081° |
| argument of perigee: | 269.3964° |
| revolutions per day: | 15.27587363 |
| mean anomaly at epoch: | 90.6553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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