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 00737U 26085.98183964 +.00000000 +00000-0 +00000-0 0 00009
2 00737 46.4661 78.1750 2602954 289.1338 44.7058 7.39537798 02
| Epoch (UTC): | 26 March 2026 23:33:50 |
| Eccentricity: | 0.2602954 |
| inclination: | 46.4661° |
| perigee height: | 1854 km |
| apogee height: | 7647 km |
| right ascension of ascending node: | 78.1750° |
| argument of perigee: | 289.1338° |
| revolutions per day: | 7.39537798 |
| mean anomaly at epoch: | 44.7058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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