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 17296U 26037.77743897 +.00000000 +00000-0 +79707-4 0 00002
2 17296 82.5309 310.0842 0016612 244.0517 115.8988 14.85599717 07
| Epoch (UTC): | 06 February 2026 18:39:30 |
| Eccentricity: | 0.0016612 |
| inclination: | 82.5309° |
| perigee height: | 600 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 310.0842° |
| argument of perigee: | 244.0517° |
| revolutions per day: | 14.85599717 |
| mean anomaly at epoch: | 115.8988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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