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 26040.24268979 +.00000000 +00000-0 +55467-4 0 00007
2 15495 82.5227 105.6206 0018681 343.3243 16.7357 14.86092132 03
| Epoch (UTC): | 09 February 2026 05:49:28 |
| Eccentricity: | 0.0018681 |
| inclination: | 82.5227° |
| perigee height: | 597 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 105.6206° |
| argument of perigee: | 343.3243° |
| revolutions per day: | 14.86092132 |
| mean anomaly at epoch: | 16.7357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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