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 20666U 26076.15313693 +.00000000 +00000-0 +14460-3 0 00003
2 20666 62.7822 228.4681 0025998 348.8451 11.2068 15.03632011 06
| Epoch (UTC): | 17 March 2026 03:40:31 |
| Eccentricity: | 0.0025998 |
| inclination: | 62.7822° |
| perigee height: | 538 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 228.4681° |
| argument of perigee: | 348.8451° |
| revolutions per day: | 15.03632011 |
| mean anomaly at epoch: | 11.2068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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