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 33490U 09001A 25358.71146050 0.00000000 00000-0 00000-0 0 09
2 33490 8.5832 33.5907 0005169 251.2747 108.6911 1.00270000 09
| Epoch (UTC): | 24 December 2025 17:04:30 |
| Eccentricity: | 0.0005169 |
| inclination: | 8.5832° |
| perigee height: | 35765 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 33.5907° |
| argument of perigee: | 251.2747° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 108.6911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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