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 03954U 26013.28088617 +.00000000 +00000-0 +00000-0 0 00006
2 03954 89.1343 29.9242 7044937 89.6246 1.2250 0.21516406 03
| Epoch (UTC): | 13 January 2026 06:44:28 |
| Eccentricity: | 0.7044937 |
| inclination: | 89.1343° |
| perigee height: | 28385 km |
| apogee height: | 194139 km |
| right ascension of ascending node: | 29.9242° |
| argument of perigee: | 89.6246° |
| revolutions per day: | 0.21516406 |
| mean anomaly at epoch: | 1.2250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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