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 67200U 26145.51590339 +.00000000 +00000-0 +12246-3 0 00009
2 67200 70.0022 340.7107 0002401 269.3870 90.7014 14.98335614 07
| Epoch (UTC): | 25 May 2026 12:22:54 |
| Eccentricity: | 0.0002401 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.7107° |
| argument of perigee: | 269.3870° |
| revolutions per day: | 14.98335614 |
| mean anomaly at epoch: | 90.7014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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