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 15495U 26039.23270797 +.00000000 +00000-0 +56433-4 0 00009
2 15495 82.5228 106.5704 0018770 346.7378 13.3342 14.86091123 08
| Epoch (UTC): | 08 February 2026 05:35:05 |
| Eccentricity: | 0.0018770 |
| inclination: | 82.5228° |
| perigee height: | 597 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 106.5704° |
| argument of perigee: | 346.7378° |
| revolutions per day: | 14.86091123 |
| mean anomaly at epoch: | 13.3342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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