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 13403U 26041.88884816 +.00000000 +00000-0 +22461-3 0 00006
2 13403 81.1445 224.7146 0024169 256.7936 103.0601 15.24399789 00
| Epoch (UTC): | 10 February 2026 21:19:56 |
| Eccentricity: | 0.0024169 |
| inclination: | 81.1445° |
| perigee height: | 476 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 224.7146° |
| argument of perigee: | 256.7936° |
| revolutions per day: | 15.24399789 |
| mean anomaly at epoch: | 103.0601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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