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 69040U 26145.58357628 +.00000000 +00000-0 -38530-2 0 00006
2 69040 97.2848 0.3776 0000719 75.2193 284.9152 15.74641852 00
| Epoch (UTC): | 25 May 2026 14:00:20 |
| Eccentricity: | 0.0000719 |
| inclination: | 97.2848° |
| perigee height: | 345 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 0.3776° |
| argument of perigee: | 75.2193° |
| revolutions per day: | 15.74641852 |
| mean anomaly at epoch: | 284.9152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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