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 13969U 26150.53537352 +.00000000 +00000-0 +00000-0 0 00008
2 13969 8.7026 320.5220 0019080 267.1914 108.3108 0.98741817 01
| Epoch (UTC): | 30 May 2026 12:50:56 |
| Eccentricity: | 0.0019080 |
| inclination: | 8.7026° |
| perigee height: | 36140 km |
| apogee height: | 36302 km |
| right ascension of ascending node: | 320.5220° |
| argument of perigee: | 267.1914° |
| revolutions per day: | 0.98741817 |
| mean anomaly at epoch: | 108.3108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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