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 00020U 26160.09803785 +.00000000 +00000-0 +12491-3 0 00000
2 00020 33.3448 296.0641 1637742 10.2110 352.7942 11.61964515 03
| Epoch (UTC): | 09 June 2026 02:21:10 |
| Eccentricity: | 0.1637742 |
| inclination: | 33.3448° |
| perigee height: | 507 km |
| apogee height: | 3204 km |
| right ascension of ascending node: | 296.0641° |
| argument of perigee: | 10.2110° |
| revolutions per day: | 11.61964515 |
| mean anomaly at epoch: | 352.7942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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