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 69002U 26145.65802584 +.00000000 +00000-0 +19746-3 0 00006
2 69002 97.7377 43.5593 0003438 71.1137 289.0455 14.92527066 01
| Epoch (UTC): | 25 May 2026 15:47:33 |
| Eccentricity: | 0.0003438 |
| inclination: | 97.7377° |
| perigee height: | 588 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 43.5593° |
| argument of perigee: | 71.1137° |
| revolutions per day: | 14.92527066 |
| mean anomaly at epoch: | 289.0455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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