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 26048.88131997 +.00000000 +00000-0 +11388-2 0 00000
2 00053 47.2796 350.3610 0098404 82.3435 278.8517 12.17402365 02
| Epoch (UTC): | 17 February 2026 21:09:06 |
| Eccentricity: | 0.0098404 |
| inclination: | 47.2796° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 350.3610° |
| argument of perigee: | 82.3435° |
| revolutions per day: | 12.17402365 |
| mean anomaly at epoch: | 278.8517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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