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 66773U 26145.18158969 +.00000000 +00000-0 +19368-3 0 00007
2 66773 97.4223 219.4100 0000581 23.9218 336.2044 15.20291250 03
| Epoch (UTC): | 25 May 2026 04:21:29 |
| Eccentricity: | 0.0000581 |
| inclination: | 97.4223° |
| perigee height: | 505 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.4100° |
| argument of perigee: | 23.9218° |
| revolutions per day: | 15.20291250 |
| mean anomaly at epoch: | 336.2044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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