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 67915U 26145.45421913 +.00000000 +00000-0 +46014-3 0 00006
2 67915 43.0018 171.6058 0001618 275.1571 84.9096 15.27587541 09
| Epoch (UTC): | 25 May 2026 10:54:04 |
| Eccentricity: | 0.0001618 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.6058° |
| argument of perigee: | 275.1571° |
| revolutions per day: | 15.27587541 |
| mean anomaly at epoch: | 84.9096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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