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 13033U 26106.27600610 +.00000000 +00000-0 +22419-4 0 00002
2 13033 82.9445 210.9668 0032119 4.4304 24.5441 13.73468652 02
| Epoch (UTC): | 16 April 2026 06:37:26 |
| Eccentricity: | 0.0032119 |
| inclination: | 82.9445° |
| perigee height: | 963 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 210.9668° |
| argument of perigee: | 4.4304° |
| revolutions per day: | 13.73468652 |
| mean anomaly at epoch: | 24.5441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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