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 27597U 26135.30708796 +.00000000 +00000-0 +71745-4 0 00008
2 27597 98.7861 94.2920 0001720 121.2643 238.8707 14.29329854 08
| Epoch (UTC): | 15 May 2026 07:22:12 |
| Eccentricity: | 0.0001720 |
| inclination: | 98.7861° |
| perigee height: | 793 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 94.2920° |
| argument of perigee: | 121.2643° |
| revolutions per day: | 14.29329854 |
| mean anomaly at epoch: | 238.8707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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