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 52669U 26145.48555541 +.00000000 +00000-0 +11576-3 0 00009
2 52669 53.2113 169.3709 0001066 61.1272 298.9827 15.08836448 04
| Epoch (UTC): | 25 May 2026 11:39:11 |
| Eccentricity: | 0.0001066 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.3709° |
| argument of perigee: | 61.1272° |
| revolutions per day: | 15.08836448 |
| mean anomaly at epoch: | 298.9827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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