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 27651U 26115.66740972 +.00000000 +00000-0 +21142-3 0 00003
2 27651 39.9899 201.2547 0016536 31.4179 328.7599 15.03418116 00
| Epoch (UTC): | 25 April 2026 16:01:04 |
| Eccentricity: | 0.0016536 |
| inclination: | 39.9899° |
| perigee height: | 545 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 201.2547° |
| argument of perigee: | 31.4179° |
| revolutions per day: | 15.03418116 |
| mean anomaly at epoch: | 328.7599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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