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 33495U 26106.22752756 +.00000000 +00000-0 +35598-4 0 00002
2 33495 98.1269 11.6585 0006672 220.7717 139.2993 14.74751129 01
| Epoch (UTC): | 16 April 2026 05:27:38 |
| Eccentricity: | 0.0006672 |
| inclination: | 98.1269° |
| perigee height: | 641 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 11.6585° |
| argument of perigee: | 220.7717° |
| revolutions per day: | 14.74751129 |
| mean anomaly at epoch: | 139.2993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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