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 67135U 26145.19412803 +.00000000 +00000-0 +43878-3 0 00004
2 67135 51.8951 75.8322 0001059 54.0050 306.1015 14.92194281 06
| Epoch (UTC): | 25 May 2026 04:39:32 |
| Eccentricity: | 0.0001059 |
| inclination: | 51.8951° |
| perigee height: | 590 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 75.8322° |
| argument of perigee: | 54.0050° |
| revolutions per day: | 14.92194281 |
| mean anomaly at epoch: | 306.1015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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