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 67216U 26145.26973477 +.00000000 +00000-0 +14343-3 0 00006
2 67216 70.0024 341.4448 0002384 268.5748 91.5138 14.98332896 02
| Epoch (UTC): | 25 May 2026 06:28:25 |
| Eccentricity: | 0.0002384 |
| inclination: | 70.0024° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.4448° |
| argument of perigee: | 268.5748° |
| revolutions per day: | 14.98332896 |
| mean anomaly at epoch: | 91.5138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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