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 67271U 26145.46796487 +.00000000 +00000-0 +18999-3 0 00004
2 67271 97.3942 220.3098 0016624 83.1956 277.1171 15.21382169 08
| Epoch (UTC): | 25 May 2026 11:13:52 |
| Eccentricity: | 0.0016624 |
| inclination: | 97.3942° |
| perigee height: | 490 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 220.3098° |
| argument of perigee: | 83.1956° |
| revolutions per day: | 15.21382169 |
| mean anomaly at epoch: | 277.1171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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