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 25115U 26088.06729882 +.00000000 +00000-0 +43456-3 0 00008
2 25115 45.0139 82.8460 0005523 242.3189 117.7102 14.46528935 06
| Epoch (UTC): | 29 March 2026 01:36:54 |
| Eccentricity: | 0.0005523 |
| inclination: | 45.0139° |
| perigee height: | 733 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 82.8460° |
| argument of perigee: | 242.3189° |
| revolutions per day: | 14.46528935 |
| mean anomaly at epoch: | 117.7102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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