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 26047.23958046 +.00000000 +00000-0 +11021-2 0 00004
2 00053 47.2796 355.4251 0098335 77.4906 283.6863 12.17401950 07
| Epoch (UTC): | 16 February 2026 05:44:59 |
| Eccentricity: | 0.0098335 |
| inclination: | 47.2796° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 355.4251° |
| argument of perigee: | 77.4906° |
| revolutions per day: | 12.17401950 |
| mean anomaly at epoch: | 283.6863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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