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 69023U 26145.65434354 +.00000000 +00000-0 +36357-3 0 00002
2 69023 97.4095 43.8782 0005037 80.0234 280.1570 15.19840450 00
| Epoch (UTC): | 25 May 2026 15:42:15 |
| Eccentricity: | 0.0005037 |
| inclination: | 97.4095° |
| perigee height: | 503 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 43.8782° |
| argument of perigee: | 80.0234° |
| revolutions per day: | 15.19840450 |
| mean anomaly at epoch: | 280.1570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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