From 63b31a4022bbfa8c4d2d0e36ef675f6ec816d467 Mon Sep 17 00:00:00 2001
From: Jorge Martinez <contact@jorgemartinez.space>
Date: Mon, 9 Sep 2024 09:07:52 +0200
Subject: [PATCH] doc: update

---
 README.md | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/README.md b/README.md
index 6a3f053..b63dcad 100644
--- a/README.md
+++ b/README.md
@@ -102,7 +102,7 @@ positions are given by:
 
 <br>
 
-The time of flight is $\Delta t = 0.010794065 \text{[year]}$. The orbit is
+The time of flight is $\Delta t = 0.010794065$ years. The orbit is
 prograde and direct, thus $M=0$. Remember that when $M=0$, there is only one
 possible solution, so the `low_path` flag does not play any role in this
 problem.