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 68974U 26145.58335647 +.00000000 +00000-0 -36170-1 0 00005
2 68974 53.1595 268.3389 0000985 77.3878 252.9314 15.53567839 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000985 |
| inclination: | 53.1595° |
| perigee height: | 406 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 268.3389° |
| argument of perigee: | 77.3878° |
| revolutions per day: | 15.53567839 |
| mean anomaly at epoch: | 252.9314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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