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 26075.14528398 +.00000000 +00000-0 +21364-3 0 00000
2 33499 98.1185 356.1387 0006724 225.4372 134.6293 14.82856186 06
| Epoch (UTC): | 16 March 2026 03:29:12 |
| Eccentricity: | 0.0006724 |
| inclination: | 98.1185° |
| perigee height: | 616 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 356.1387° |
| argument of perigee: | 225.4372° |
| revolutions per day: | 14.82856186 |
| mean anomaly at epoch: | 134.6293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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