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 13720U 26088.16909700 +.00000000 +00000-0 +54469-4 0 00004
2 13720 81.2475 64.3514 0055233 183.9718 193.0066 14.16006605 04
| Epoch (UTC): | 29 March 2026 04:03:29 |
| Eccentricity: | 0.0055233 |
| inclination: | 81.2475° |
| perigee height: | 799 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 64.3514° |
| argument of perigee: | 183.9718° |
| revolutions per day: | 14.16006605 |
| mean anomaly at epoch: | 193.0066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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