▸Orbital parameters

Orbit class	SSO
Inclination	97.3810°
Eccentricity	0.0003069
Period	93.9 min
Apogee	469 km
Perigee	465 km
Mean motion	15.33055957 rev/day
RAAN	268.6719°
Arg of perigee	171.0564°
Mean anomaly	189.0733°
B*	2.0945e-4
Rev at epoch	10,508

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60485U 24149T 26187.75043016 .00006610 00000-0 20945-3 0 9999

2 60485 97.3810 268.6719 0003069 171.0564 189.0733 15.33055957105082

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TOMORROW-S2",
  "OBJECT_ID": "2024-149T",
  "EPOCH": "2026-07-06T18:00:37.166+00:00",
  "MEAN_MOTION": 15.33055957,
  "ECCENTRICITY": 0.0003069,
  "INCLINATION": 97.381,
  "RA_OF_ASC_NODE": 268.6719,
  "ARG_OF_PERICENTER": 171.0564,
  "MEAN_ANOMALY": 189.0733,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60485,
  "REV_AT_EPOCH": 10508,
  "BSTAR": 0.00020945,
  "MEAN_MOTION_DOT": 0.0000661,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	TOMORROW-S2
Operator	Tomorrow.io (The Tomorrow Companies Inc.)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/60485

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.