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 67744U 26145.58071243 +.00000000 +00000-0 +72921-3 0 00003
2 67744 97.2861 199.1587 0000302 130.8233 229.3036 15.33451895 07
| Epoch (UTC): | 25 May 2026 13:56:13 |
| Eccentricity: | 0.0000302 |
| inclination: | 97.2861° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.1587° |
| argument of perigee: | 130.8233° |
| revolutions per day: | 15.33451895 |
| mean anomaly at epoch: | 229.3036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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