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 68449U 26145.42246567 +.00000000 +00000-0 +35664-3 0 00005
2 68449 97.4495 104.1502 0005203 131.5226 228.6455 15.17721539 07
| Epoch (UTC): | 25 May 2026 10:08:21 |
| Eccentricity: | 0.0005203 |
| inclination: | 97.4495° |
| perigee height: | 509 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 104.1502° |
| argument of perigee: | 131.5226° |
| revolutions per day: | 15.17721539 |
| mean anomaly at epoch: | 228.6455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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