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 31699U 26037.53496397 +.00000000 +00000-0 +30011-3 0 00003
2 31699 97.4463 23.4295 0334807 44.9070 64.5398 14.45738396 02
| Epoch (UTC): | 06 February 2026 12:50:20 |
| Eccentricity: | 0.0334807 |
| inclination: | 97.4463° |
| perigee height: | 501 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 23.4295° |
| argument of perigee: | 44.9070° |
| revolutions per day: | 14.45738396 |
| mean anomaly at epoch: | 64.5398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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