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 00733U 26088.05867646 +.00000000 +00000-0 +95000-4 0 00000
2 00733 99.1214 102.4516 0032574 200.4630 159.5250 14.34030182 09
| Epoch (UTC): | 29 March 2026 01:24:29 |
| Eccentricity: | 0.0032574 |
| inclination: | 99.1214° |
| perigee height: | 755 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 102.4516° |
| argument of perigee: | 200.4630° |
| revolutions per day: | 14.34030182 |
| mean anomaly at epoch: | 159.5250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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