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 26041.62219036 +.00000000 +00000-0 +49161-4 0 00006
2 13778 100.0819 79.3064 0020205 263.4823 96.4042 14.09686424 02
| Epoch (UTC): | 10 February 2026 14:55:57 |
| Eccentricity: | 0.0020205 |
| inclination: | 100.0819° |
| perigee height: | 846 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 79.3064° |
| argument of perigee: | 263.4823° |
| revolutions per day: | 14.09686424 |
| mean anomaly at epoch: | 96.4042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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