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 06324U 26074.03388552 +.00000000 +00000-0 +98641-4 0 00003
2 06324 74.0762 304.3125 0008830 334.7576 25.3150 14.45283835 04
| Epoch (UTC): | 15 March 2026 00:48:47 |
| Eccentricity: | 0.0008830 |
| inclination: | 74.0762° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 304.3125° |
| argument of perigee: | 334.7576° |
| revolutions per day: | 14.45283835 |
| mean anomaly at epoch: | 25.3150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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