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 68737U 26145.58335647 +.00000000 +00000-0 -28634-1 0 00008
2 68737 97.2850 9.2420 0001457 94.0956 253.7464 15.57252603 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001457 |
| inclination: | 97.2850° |
| perigee height: | 395 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 9.2420° |
| argument of perigee: | 94.0956° |
| revolutions per day: | 15.57252603 |
| mean anomaly at epoch: | 253.7464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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