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 10121U 26088.14897148 +.00000000 +00000-0 +10689-3 0 00001
2 10121 74.0488 5.8687 0019499 284.0099 75.8887 14.37370040 08
| Epoch (UTC): | 29 March 2026 03:34:31 |
| Eccentricity: | 0.0019499 |
| inclination: | 74.0488° |
| perigee height: | 753 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 5.8687° |
| argument of perigee: | 284.0099° |
| revolutions per day: | 14.37370040 |
| mean anomaly at epoch: | 75.8887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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