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 26042.12798758 +.00000000 +00000-0 +49126-4 0 00004
2 15495 82.5223 103.8476 0018512 336.9147 23.1235 14.86093771 09
| Epoch (UTC): | 11 February 2026 03:04:18 |
| Eccentricity: | 0.0018512 |
| inclination: | 82.5223° |
| perigee height: | 597 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 103.8476° |
| argument of perigee: | 336.9147° |
| revolutions per day: | 14.86093771 |
| mean anomaly at epoch: | 23.1235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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