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 15378U 26041.41071826 +.00000000 +00000-0 +26720-4 0 00000
2 15378 64.9927 29.5162 0036954 11.2563 348.9315 13.83704629 09
| Epoch (UTC): | 10 February 2026 09:51:26 |
| Eccentricity: | 0.0036954 |
| inclination: | 64.9927° |
| perigee height: | 924 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 29.5162° |
| argument of perigee: | 11.2563° |
| revolutions per day: | 13.83704629 |
| mean anomaly at epoch: | 348.9315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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