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 39446U 26032.40909676 +.00000000 +00000-0 +44808-3 0 00000
2 39446 97.8536 347.8289 0051854 53.5101 307.0880 14.95686645 05
| Epoch (UTC): | 01 February 2026 09:49:05 |
| Eccentricity: | 0.0051854 |
| inclination: | 97.8536° |
| perigee height: | 544 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 347.8289° |
| argument of perigee: | 53.5101° |
| revolutions per day: | 14.95686645 |
| mean anomaly at epoch: | 307.0880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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