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 26038.00243131 +.00000000 +00000-0 +53771-4 0 00009
2 13778 100.0822 75.2566 0020157 273.5745 86.3116 14.09685642 00
| Epoch (UTC): | 07 February 2026 00:03:30 |
| Eccentricity: | 0.0020157 |
| inclination: | 100.0822° |
| perigee height: | 846 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 75.2566° |
| argument of perigee: | 273.5745° |
| revolutions per day: | 14.09685642 |
| mean anomaly at epoch: | 86.3116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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