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 00115U 26088.13239154 +.00000000 +00000-0 +37617-3 0 00009
2 00115 48.1618 134.5909 0027310 258.3972 101.3881 14.97710123 04
| Epoch (UTC): | 29 March 2026 03:10:38 |
| Eccentricity: | 0.0027310 |
| inclination: | 48.1618° |
| perigee height: | 555 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 134.5909° |
| argument of perigee: | 258.3972° |
| revolutions per day: | 14.97710123 |
| mean anomaly at epoch: | 101.3881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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