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 13533U 26063.42886706 +.00000000 +00000-0 +11074-2 0 00001
2 13533 101.8542 38.9161 0361058 86.7481 61.8137 11.74564638 04
| Epoch (UTC): | 04 March 2026 10:17:34 |
| Eccentricity: | 0.0361058 |
| inclination: | 101.8542° |
| perigee height: | 1502 km |
| apogee height: | 2092 km |
| right ascension of ascending node: | 38.9161° |
| argument of perigee: | 86.7481° |
| revolutions per day: | 11.74564638 |
| mean anomaly at epoch: | 61.8137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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