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 26137.85133236 +.00000000 +00000-0 -38742-4 0 00003
2 23088 71.0003 285.6389 0004383 223.7928 136.2848 14.15023107 02
| Epoch (UTC): | 17 May 2026 20:25:55 |
| Eccentricity: | 0.0004383 |
| inclination: | 71.0003° |
| perigee height: | 839 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 285.6389° |
| argument of perigee: | 223.7928° |
| revolutions per day: | 14.15023107 |
| mean anomaly at epoch: | 136.2848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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