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 61776U 26145.58632854 +.00000000 +00000-0 +66794-3 0 00004
2 61776 97.2933 21.5791 0006848 32.9180 327.2501 15.58205715 05
| Epoch (UTC): | 25 May 2026 14:04:18 |
| Eccentricity: | 0.0006848 |
| inclination: | 97.2933° |
| perigee height: | 388 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 21.5791° |
| argument of perigee: | 32.9180° |
| revolutions per day: | 15.58205715 |
| mean anomaly at epoch: | 327.2501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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