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 40878U 26145.60241059 +.00000000 +00000-0 -56646-3 0 00006
2 40878 100.1151 132.9667 0007444 267.7521 92.2740 13.16068754 06
| Epoch (UTC): | 25 May 2026 14:27:28 |
| Eccentricity: | 0.0007444 |
| inclination: | 100.1151° |
| perigee height: | 1194 km |
| apogee height: | 1205 km |
| right ascension of ascending node: | 132.9667° |
| argument of perigee: | 267.7521° |
| revolutions per day: | 13.16068754 |
| mean anomaly at epoch: | 92.2740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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