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 67483U 26145.46022052 +.00000000 +00000-0 +94449-4 0 00004
2 67483 97.5246 216.7428 0011144 191.3414 168.7560 14.97480937 02
| Epoch (UTC): | 25 May 2026 11:02:43 |
| Eccentricity: | 0.0011144 |
| inclination: | 97.5246° |
| perigee height: | 567 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 216.7428° |
| argument of perigee: | 191.3414° |
| revolutions per day: | 14.97480937 |
| mean anomaly at epoch: | 168.7560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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