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 17295U 26065.13056456 +.00000000 +00000-0 +14059-3 0 00008
2 17295 82.4628 199.5909 0011771 272.0058 87.9898 16.49575463 08
| Epoch (UTC): | 06 March 2026 03:08:00 |
| Eccentricity: | 0.0011771 |
| inclination: | 82.4628° |
| perigee height: | 133 km |
| apogee height: | 148 km |
| right ascension of ascending node: | 199.5909° |
| argument of perigee: | 272.0058° |
| revolutions per day: | 16.49575463 |
| mean anomaly at epoch: | 87.9898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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