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 00053U 26039.35920044 +.00000000 +00000-0 +61961-4 0 00005
2 00053 47.2793 19.7324 0098091 54.1988 306.7870 12.17401100 08
| Epoch (UTC): | 08 February 2026 08:37:14 |
| Eccentricity: | 0.0098091 |
| inclination: | 47.2793° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 19.7324° |
| argument of perigee: | 54.1988° |
| revolutions per day: | 12.17401100 |
| mean anomaly at epoch: | 306.7870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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