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 69102U 26135.87795279 +.00000000 +00000-0 +13375-3 0 00004
2 69102 97.5061 218.5961 0181468 13.3087 347.2857 15.50517461 01
| Epoch (UTC): | 15 May 2026 21:04:15 |
| Eccentricity: | 0.0181468 |
| inclination: | 97.5061° |
| perigee height: | 292 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 218.5961° |
| argument of perigee: | 13.3087° |
| revolutions per day: | 15.50517461 |
| mean anomaly at epoch: | 347.2857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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