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 68588U 26145.58335647 +.00000000 +00000-0 -80362-2 0 00009
2 68588 51.8980 293.1017 0001837 156.2549 268.0458 14.80325955 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001837 |
| inclination: | 51.8980° |
| perigee height: | 627 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 293.1017° |
| argument of perigee: | 156.2549° |
| revolutions per day: | 14.80325955 |
| mean anomaly at epoch: | 268.0458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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