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 66821U 26145.34653255 +.00000000 +00000-0 -40537-4 0 00001
2 66821 70.0006 141.3708 0003172 268.5542 91.5254 14.98332833 07
| Epoch (UTC): | 25 May 2026 08:19:00 |
| Eccentricity: | 0.0003172 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 141.3708° |
| argument of perigee: | 268.5542° |
| revolutions per day: | 14.98332833 |
| mean anomaly at epoch: | 91.5254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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