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 69017U 26145.58074892 +.00000000 +00000-0 +12415-4 0 00004
2 69017 97.4076 43.8150 0004710 89.7824 270.3951 15.20683256 04
| Epoch (UTC): | 25 May 2026 13:56:16 |
| Eccentricity: | 0.0004710 |
| inclination: | 97.4076° |
| perigee height: | 501 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 43.8150° |
| argument of perigee: | 89.7824° |
| revolutions per day: | 15.20683256 |
| mean anomaly at epoch: | 270.3951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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