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 67740U 26145.12936416 +.00000000 +00000-0 +37503-3 0 00008
2 67740 97.2844 198.7032 0001190 93.1156 267.0223 15.33452003 04
| Epoch (UTC): | 25 May 2026 03:06:17 |
| Eccentricity: | 0.0001190 |
| inclination: | 97.2844° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.7032° |
| argument of perigee: | 93.1156° |
| revolutions per day: | 15.33452003 |
| mean anomaly at epoch: | 267.0223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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