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 00012U 26041.12346877 +.00000000 +00000-0 +37593-3 0 00007
2 00012 32.9003 313.0523 1646700 152.2389 217.6801 11.48528722 08
| Epoch (UTC): | 10 February 2026 02:57:47 |
| Eccentricity: | 0.1646700 |
| inclination: | 32.9003° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 313.0523° |
| argument of perigee: | 152.2389° |
| revolutions per day: | 11.48528722 |
| mean anomaly at epoch: | 217.6801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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