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 53969U 26145.53798368 +.00000000 +00000-0 +61702-4 0 00002
2 53969 53.2158 239.1306 0001137 90.8536 269.2586 15.08840862 05
| Epoch (UTC): | 25 May 2026 12:54:41 |
| Eccentricity: | 0.0001137 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.1306° |
| argument of perigee: | 90.8536° |
| revolutions per day: | 15.08840862 |
| mean anomaly at epoch: | 269.2586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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