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 68363U 26145.15094659 +.00000000 +00000-0 +54482-3 0 00002
2 68363 82.2968 37.4155 0019875 181.6102 178.5120 16.08971499 05
| Epoch (UTC): | 25 May 2026 03:37:21 |
| Eccentricity: | 0.0019875 |
| inclination: | 82.2968° |
| perigee height: | 236 km |
| apogee height: | 263 km |
| right ascension of ascending node: | 37.4155° |
| argument of perigee: | 181.6102° |
| revolutions per day: | 16.08971499 |
| mean anomaly at epoch: | 178.5120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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