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 15755U 26064.20928709 +.00000000 +00000-0 +54228-4 0 00006
2 15755 71.1115 135.4104 0033935 149.2127 211.1000 14.20989676 05
| Epoch (UTC): | 05 March 2026 05:01:22 |
| Eccentricity: | 0.0033935 |
| inclination: | 71.1115° |
| perigee height: | 798 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 135.4104° |
| argument of perigee: | 149.2127° |
| revolutions per day: | 14.20989676 |
| mean anomaly at epoch: | 211.1000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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