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 00537U 26070.84422046 +.00000000 +00000-0 +50488-3 0 00001
2 00537 67.2287 342.0635 0174254 2.5641 57.4124 13.65029755 09
| Epoch (UTC): | 11 March 2026 20:15:40 |
| Eccentricity: | 0.0174254 |
| inclination: | 67.2287° |
| perigee height: | 889 km |
| apogee height: | 1146 km |
| right ascension of ascending node: | 342.0635° |
| argument of perigee: | 2.5641° |
| revolutions per day: | 13.65029755 |
| mean anomaly at epoch: | 57.4124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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