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 20663U 26074.89842130 +.00000000 +00000-0 +15430-3 0 00000
2 20663 62.7912 314.4026 0016095 191.6954 168.3775 15.05687981 09
| Epoch (UTC): | 15 March 2026 21:33:43 |
| Eccentricity: | 0.0016095 |
| inclination: | 62.7912° |
| perigee height: | 538 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 314.4026° |
| argument of perigee: | 191.6954° |
| revolutions per day: | 15.05687981 |
| mean anomaly at epoch: | 168.3775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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