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 36501U 26074.28581409 +.00000000 +00000-0 +11280-2 0 00008
2 36501 49.6491 279.0399 4793958 90.1811 322.6825 5.96717647 04
| Epoch (UTC): | 15 March 2026 06:51:34 |
| Eccentricity: | 0.4793958 |
| inclination: | 49.6491° |
| perigee height: | 306 km |
| apogee height: | 12617 km |
| right ascension of ascending node: | 279.0399° |
| argument of perigee: | 90.1811° |
| revolutions per day: | 5.96717647 |
| mean anomaly at epoch: | 322.6825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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