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 68277U 26145.48692267 +.00000000 +00000-0 +85652-3 0 00004
2 68277 53.1593 321.4904 0001562 88.6022 271.5160 15.34405329 09
| Epoch (UTC): | 25 May 2026 11:41:10 |
| Eccentricity: | 0.0001562 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 321.4904° |
| argument of perigee: | 88.6022° |
| revolutions per day: | 15.34405329 |
| mean anomaly at epoch: | 271.5160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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