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 13719U 26088.13765861 +.00000000 +00000-0 +54591-4 0 00003
2 13719 81.2503 97.9083 0070798 201.6440 225.9488 14.15181530 03
| Epoch (UTC): | 29 March 2026 03:18:13 |
| Eccentricity: | 0.0070798 |
| inclination: | 81.2503° |
| perigee height: | 791 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 97.9083° |
| argument of perigee: | 201.6440° |
| revolutions per day: | 14.15181530 |
| mean anomaly at epoch: | 225.9488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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