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 53669U 26145.66668980 +.00000000 +00000-0 +21399-2 0 00005
2 53669 97.6037 27.5637 0001766 80.3045 301.9223 15.38090358 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001766 |
| inclination: | 97.6037° |
| perigee height: | 451 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 27.5637° |
| argument of perigee: | 80.3045° |
| revolutions per day: | 15.38090358 |
| mean anomaly at epoch: | 301.9223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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