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 33499U 26102.20324948 +.00000000 +00000-0 +13194-3 0 00005
2 33499 98.1188 23.6112 0008761 136.4231 223.7676 14.82954873 06
| Epoch (UTC): | 12 April 2026 04:52:40 |
| Eccentricity: | 0.0008761 |
| inclination: | 98.1188° |
| perigee height: | 614 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 23.6112° |
| argument of perigee: | 136.4231° |
| revolutions per day: | 14.82954873 |
| mean anomaly at epoch: | 223.7676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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