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 68284U 26145.22696034 +.00000000 +00000-0 +77288-3 0 00006
2 68284 53.1602 324.8832 0001435 103.2403 256.8760 15.34396398 08
| Epoch (UTC): | 25 May 2026 05:26:49 |
| Eccentricity: | 0.0001435 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 324.8832° |
| argument of perigee: | 103.2403° |
| revolutions per day: | 15.34396398 |
| mean anomaly at epoch: | 256.8760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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