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 67260U 26145.11557597 +.00000000 +00000-0 +27481-3 0 00007
2 67260 97.3955 220.0240 0015379 86.8121 273.4874 15.21807243 00
| Epoch (UTC): | 25 May 2026 02:46:25 |
| Eccentricity: | 0.0015379 |
| inclination: | 97.3955° |
| perigee height: | 490 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 220.0240° |
| argument of perigee: | 86.8121° |
| revolutions per day: | 15.21807243 |
| mean anomaly at epoch: | 273.4874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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