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 33496U 26150.71919154 +.00000000 +00000-0 +10128-3 0 00004
2 33496 98.1413 55.3453 0007201 74.5277 285.6726 14.75005437 02
| Epoch (UTC): | 30 May 2026 17:15:38 |
| Eccentricity: | 0.0007201 |
| inclination: | 98.1413° |
| perigee height: | 640 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 55.3453° |
| argument of perigee: | 74.5277° |
| revolutions per day: | 14.75005437 |
| mean anomaly at epoch: | 285.6726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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