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 67275U 26145.15241559 +.00000000 +00000-0 +27956-3 0 00002
2 67275 97.3913 220.0728 0015382 90.1179 270.1820 15.22271362 09
| Epoch (UTC): | 25 May 2026 03:39:28 |
| Eccentricity: | 0.0015382 |
| inclination: | 97.3913° |
| perigee height: | 488 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.0728° |
| argument of perigee: | 90.1179° |
| revolutions per day: | 15.22271362 |
| mean anomaly at epoch: | 270.1820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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