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 69095U 26145.59196822 +.00000000 +00000-0 +48749-3 0 00007
2 69095 88.9782 197.3315 0482868 24.2874 338.0315 15.09137822 06
| Epoch (UTC): | 25 May 2026 14:12:26 |
| Eccentricity: | 0.0482868 |
| inclination: | 88.9782° |
| perigee height: | 205 km |
| apogee height: | 873 km |
| right ascension of ascending node: | 197.3315° |
| argument of perigee: | 24.2874° |
| revolutions per day: | 15.09137822 |
| mean anomaly at epoch: | 338.0315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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