Still Testing

 2018-010A

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The second launch carried three cubesats - two Lemurs and one Dove.

Date	Time	Event	Orbit
2018 Jan 21	0143	Launch by Electron	RL LC1
		T+2:30 Stage 1 MECO
		T+2:34 Stage 1 sep
		T+2:36 Stage 2 burn
	0146	T+3:04 Fairing
		T+6:38 Eject 2 turbopump batteries 4.6 km/s
	0151	T+8:14 St 2 MECO
	0151	T+8:31 Payload separation	300 x 500 x 83
	0233	T+50m Stage 3 burn apogee over 30N 15W