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 68084U 26145.48168723 +.00000000 +00000-0 +77289-3 0 00002
2 68084 53.1586 181.2304 0001213 81.2933 278.8207 15.34391763 04
| Epoch (UTC): | 25 May 2026 11:33:37 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.2304° |
| argument of perigee: | 81.2933° |
| revolutions per day: | 15.34391763 |
| mean anomaly at epoch: | 278.8207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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