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 23088U 26075.64271594 +.00000000 +00000-0 -31971-4 0 00008
2 23088 70.9990 56.2836 0005572 278.8188 81.2304 14.15010026 06
| Epoch (UTC): | 16 March 2026 15:25:30 |
| Eccentricity: | 0.0005572 |
| inclination: | 70.9990° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 56.2836° |
| argument of perigee: | 278.8188° |
| revolutions per day: | 14.15010026 |
| mean anomaly at epoch: | 81.2304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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