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 69018U 26145.64830588 +.00000000 +00000-0 +11439-3 0 00008
2 69018 97.4071 43.8755 0006379 97.7966 262.3993 15.20167748 00
| Epoch (UTC): | 25 May 2026 15:33:33 |
| Eccentricity: | 0.0006379 |
| inclination: | 97.4071° |
| perigee height: | 501 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 43.8755° |
| argument of perigee: | 97.7966° |
| revolutions per day: | 15.20167748 |
| mean anomaly at epoch: | 262.3993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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