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 26075.07216543 +.00000000 +00000-0 +94772-4 0 00009
2 06324 74.0760 302.3822 0008859 332.7585 27.3107 14.45284486 00
| Epoch (UTC): | 16 March 2026 01:43:55 |
| Eccentricity: | 0.0008859 |
| inclination: | 74.0760° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 302.3822° |
| argument of perigee: | 332.7585° |
| revolutions per day: | 14.45284486 |
| mean anomaly at epoch: | 27.3107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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