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 67872U 26145.46752700 +.00000000 +00000-0 +65545-3 0 00000
2 67872 53.1573 207.4044 0001046 89.0581 271.0540 15.30191739 07
| Epoch (UTC): | 25 May 2026 11:13:14 |
| Eccentricity: | 0.0001046 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.4044° |
| argument of perigee: | 89.0581° |
| revolutions per day: | 15.30191739 |
| mean anomaly at epoch: | 271.0540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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