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 13778U 26088.11113838 +.00000000 +00000-0 +99323-4 0 00009
2 13778 100.0728 131.2981 0021497 136.7392 223.5467 14.09697400 04
| Epoch (UTC): | 29 March 2026 02:40:02 |
| Eccentricity: | 0.0021497 |
| inclination: | 100.0728° |
| perigee height: | 845 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 131.2981° |
| argument of perigee: | 136.7392° |
| revolutions per day: | 14.09697400 |
| mean anomaly at epoch: | 223.5467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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