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 10033U 26150.53750145 +.00000000 +00000-0 +12481-3 0 00003
2 10033 99.1181 198.0605 0036661 279.7890 79.9152 14.31453932 09
| Epoch (UTC): | 30 May 2026 12:54:00 |
| Eccentricity: | 0.0036661 |
| inclination: | 99.1181° |
| perigee height: | 761 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 198.0605° |
| argument of perigee: | 279.7890° |
| revolutions per day: | 14.31453932 |
| mean anomaly at epoch: | 79.9152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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